04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
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<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10<strong>01</strong>6913 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>294 FAA STC SR02131NY-D SIKORSKY S-76A<br />
Installation of Keystone Helicopter Corporation Prior to installation of this modification the<br />
26.07.2007<br />
SIKORSKY S-76B<br />
Deluxe VIP Interior.<br />
installer must determine that the<br />
SIKORSKY S-76C<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
10<strong>01</strong>6914 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>295 FAA STC SR02130NY-D SIKORSKY S-76A<br />
SIKORSKY S-76B<br />
SIKORSKY S-76C<br />
10<strong>01</strong>6915 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>296 FAA STC SR02123NY-D SIKORSKY S-76A<br />
SIKORSKY S-76B<br />
SIKORSKY S-76C<br />
10<strong>01</strong>6916 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>297 FAA STC SR02122NY-D SIKORSKY S-76A<br />
SIKORSKY S-76B<br />
SIKORSKY S-76C<br />
Installation of Garmin GMX 200 Multi Function<br />
Display. This STC has been classified as<br />
"BASIC" by the FAA and has been approved<br />
under the PTVP. The flight manual has been<br />
reviewed and is acceptable.<br />
Installation of Provisions for a EuroAvionics<br />
EuroNav IV System. STC SR02123NY-D<br />
classified as Basic by the FAA through FAA<br />
Order 8110.52.<br />
Installation of High Intensity Strobe Lights. STC<br />
Classified as Basic by FAA.<br />
10<strong>01</strong>6946 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>340 FAA STC SR<strong>01</strong>976NY-D SIKORSKY S-92A Installation of Keystone Helicopter Auxiliary<br />
Gauges and Relocation of Fill Ports for the Low<br />
Float Pressure Warning System.<br />
10<strong>01</strong>6981 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>384 FAA STC SR02417NY-D SIKORSKY S-76A<br />
SIKORSKY S-76B<br />
SIKORSKY S-76C<br />
10<strong>01</strong>6982 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>386<br />
REVISION 1<br />
10<strong>01</strong>6983 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>387 FAA STC SR02426NY-D SIKORSKY S-76A<br />
SIKORSKY S-76B<br />
SIKORSKY S-76C<br />
Installation of Honeywell KHF 1050 HF<br />
Communication System.<br />
FAA STC SR02152NY-D SIKORSKY S-92A Installation of a Cockpit Pressure Refuelling<br />
Control in a Sikorsky S-92A. This STC has<br />
been classified as "BASIC" by the FAA and has<br />
been approved under the PTVP.<br />
Installation of a Replacement Concorde Lead<br />
Acid Battery.<br />
10<strong>01</strong>6997 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>406 REV. 1 FAA STC02436NY-D SIKORSKY S-92A Installation of a High Intensity Strobe Lights.<br />
This STC has been classified as BASIC by the<br />
FAA and has been approved under the PTVP.<br />
10<strong>01</strong>7<strong>01</strong>8 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>436 REV. 1 FAA STC SR<strong>01</strong>949NY-D EUROCOPTER FRANCE AS<br />
365N1<br />
EUROCOPTER FRANCE AS<br />
365N2<br />
EUROCOPTER FRANCE AS<br />
365N3<br />
Installation of a Honeywell Chadwick Model<br />
15175 VXP System.<br />
10<strong>01</strong>7<strong>04</strong>0 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>464 FAA STC SR02435NY-D SIKORSKY S-92A Installation of a Rockwell Collins SAR-126<br />
Direction Finder System. This STC has been<br />
classified as “BASIC” by the FAA and has<br />
beenapproved under the PTVP.<br />
The FAA has not certified, and <strong>EASA</strong> has not<br />
validated, the equipment for which these<br />
provisions are intended. Additional approvals<br />
are required to install this equipment. The<br />
equipment installation must be evaluated to<br />
ensure that it complies with the appl<br />
03.07.2007<br />
19.03.2007<br />
15.03.2007<br />
29.06.2007<br />
Refer to FAA STC SR02417NY-D. <strong>04</strong>.12.2007<br />
none 1. Prior to installation of this<br />
modification the installer mustdetermine<br />
that the interrelationship between this<br />
modification and anyother previously<br />
installed modification will introduce no<br />
adverse effectupon the airworthiness of<br />
the product;2. The<br />
Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
10<strong>01</strong>7070 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>506 FAA STC SR02577NY-D SIKORSKY S-76C Keystone Helicopters STC SR02577NY-D; 1. Prior to installation of this modification the<br />
Introduction of a cockpit digital video recorder installer must determine that the<br />
system to meet JAR-OPS 3 flight data interrelationship between this modification and<br />
recorder requirements on applicable Sikorsky S-any<br />
other previously installed modification will<br />
76C series aircraft.<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The i<br />
10<strong>01</strong>7076 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>519 FAA STC SR02573NY-D SIKORSKY S-92A Installation of Main Rotor Blade Recognition 1. Prior to installation of this modification the<br />
Lights.<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product.2.<br />
10<strong>01</strong>7083 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>550 FAA STC SR02208NY-D SIKORSKY S-92A Installation of lavatory. 1. Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product.2.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 406/<strong>462</strong><br />
09.11.2007<br />
05.02.2008<br />
19.03.2008<br />
29.06.2<strong>01</strong>1<br />
10.07.2008<br />
19.02.2009<br />
02.12.2008<br />
30.<strong>04</strong>.2009